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THIS IS SEGMENT 27 COVERING CHAPTER 28.

TECHNICAL ORDER 00-105E-9 TECHNICAL CONTENT MANAGER

WRITTEN CORRESPONDENCE:

HQ AFCESA/CEXFATTN: Fire and Emergency Services Egress Manager139 Barnes Drive Suite 1Tyndall AFB, Florida 32403-5319

E-MAIL: [email protected]

INTERNET: HQ AFCESA Fire and Emergency Services PUBLIC WEB PAGE: http://www.afcesa.af.mil/CEX/cexf/index.asp Safety Supplements: http://www.afcesa.af.mil/CEX/cexf/_firemgt.asp

PHONE: (850) 283-6150DSN 523-6150

FAX: (850) 283-6383DSN 523-6383

For technical order improvements, correcting procedures, and other inquiries,please use the above media most convenient.

This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the currentRevision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> forquick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for hisoperation. Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies. If the user printsout pages his unit requires, the user shall print the affected page(s), remove and destroy the existing page(s), and insert the newly printedpage(s) in the binder provided for that purpose. A Master of this TO shall be retained in the unit’s library for reference, future printingrequirements and inspections.

CHAPTER AIRCRAFT PAGE EXPLANATION OF CHANGE

SEGMENT 27 INFORMATION CHANGE NOTICE

None.

TO 00-105E-9

Chapter 28 Cover

NOTE

Chapter 28 contains emergency rescue andmishap response information for the following NATO aircraft:

FRA, CAN AIRBUS A310-300/CC-150 GEU AIRBUS A310-304 GBR ANDOVER CC2

ESP, PRT, USA AVIOCAR 212 GBR BAE 146 BEL BN 2A

DNK, ITA, TUR C-20/HUSA, ITA C-27A/G222

USA, NLD C-31A/F-27CAN, TUR CC-129/C-47

MULTI-NATION C-130/T-10 FRA C-130H

MULTI-NATION C-135 FRA C-135 FR GEU C-140

FRA, GEU, TUR C-160 TRANSALL ASTARTE FRA C-160 TRANSALL GABRIELCAN, USA CC-138/UV-18A/BCAN, USA CC-142/E-9A CAN CC/CE/CP-144FRA, ESP CN-235 NLD DO-28 NLD FOKKER 60BEL, GBR 748 HAWKER SIDDELEY GRE HU-16B FRA NORD 262** GBR TRISTAR C2/C2K GRE YS-11A

* Aircraft information pending** Aircraft removed from inventory

T.O. 00-105E-9

28-1. INTRODUCTION AND USE.

28-2. This section contains emergency rescue andmishap response information illustrations in alpha-numerical order relative to type and model of aircraft.This arrangement of illustrations is maintained fromChapter 4 throughout the remainder of the publica-tion.

28-3. GENERAL ARRANGEMENT.

28-4. Aircraft type designation has been positionedin the upper right corner of the horizontal illustrationfor rapid identification. Additional aids to rapid orien-tation are:

a. Recent technological advances in avia-tion have caused concern for the modern firefighter.Aircraft hazards, cabin configurations, airframe ma-terials, and any other information that would be help-ful in fighting fires, the locating and rescue of per-sonnel will be added as the information becomesavailable.

b. Suggested special tools/equipment arelisted in the upper left corner, on the Aircraft/Entrypage of each listed aircraft.

c. Procedural steps covering emergency/normal entrances, cut-ins, engine/APU shutdown,safetying ejection/escape systems, and aircrew ex-traction are outlined on the left side of each pagewith coordinated illustrations on the right.

d. Illustrations located on right side of pagesare coordinated with text by numerals and small let-ters depicting both paragraph and subparagraph onthe page.

e. Each illustration is consistently coloredand/or pattern keyed to highlight essential emergencyrescue information.

f. Details are pulled directly from the illus-tration to highlight an area, thus eliminating unnec-essary searching for desired information.

CHAPTER 28

NATO

CARGO

AEROSPACE EMERGENCY RESCUEAND MISHAP RESPONSE INFORMATION

28-1

AIRBUS A310-300T.O

. 00-105E-9

AIR

BU

S A

310-300.

AIRCRAFT HAZARDS

1

HYDRAULIC OIL

FUEL F.3420,090 US GAL(76,050 LITRES)

OXYGEN

BATTERY

NOTE: This Airbus A310-300 is also known as the Canadian CC-150 Polaris.

AIRCRAFT DIMENSIONS

WING SPAN 144’ 0” (43.89 M)LENGTH 153’ 1” (46.66 M)HEIGHT 51’ 10” (15.80 M)

NOTE: The Airbus 310-300 is an extended range airliner. Additonal fuel tanks can be added to the lower cargo area to extend range or it can be configured as a cargo carrier.

ACCOMODATION: Crew of two on flight deck. It has provisions for third and fourth crew seats. Typical seating is 20 first class and 200 economy class. Aircraft is certified up to 280 people.

ARMAMENT: None carried.

AIRBUS A310-300T.O

. 00-105E-9

AIR

BU

S A

310-300.2

AIRCRAFT HAZARDS-Continued

6’ (1.80 M)

ENGINE AT FULL POWER 50’ (15.25 M)

ENGINE AT IDLE POWER 27’ (7.52 M)

5’ (1.50 M)

36’ (11.2 M) 169 KM/H 91 KT

55’ (16.8 M)105 KM/H 57 KT

180’ (54.9 M)35 KM/H 17 KT

40

15

0

0

160’ (48.8 M)169 KM/H 91 KT

90’ (27.4 M)233 KM/H 120 KT

60’ (18.3 M)338 KM/H 182 KT

AIRBUS A310-300T.O

. 00-105E-9

AIR

BU

S A

310-300.3

SPECIAL TOOLS/EQUIPMENTSkin Penetration ToolPower Rescue SawCrash AxAIRCRAFT ENTRY

1. FRONT, AFT, AND EMERGENCY DOORS

a. Reach hand into hatch “a”.b. Hold and pull handle “b” to the horizontal position. (Green line appears.)c. Open front and aft doors in the forward direction of the aircraft.d. Open emergency exits from up to down.

NOTE: A red flashing light in front or aft door windows indicates a residual pressure inside the cabin. Opening from outside automatically neutralizes the slide deployment.

2. FRONT AND AFT CARGO DOOR - RIGHT SIDE

a. Unlock doors by pressing pushbutton “c”.b. Pull handle “d” downwards.c. Opening doors, green indicator “e” is lighted.d. Set and hold selector “f” on open for at least 3 seconds.e. Open doors to upper lock.

3. BULK DOOR - AFT RIGHT SIDE

a. Pree button “g”.b. Hold and turn handle “h”.c. Push door inside.d. Reset handle in initial position.e. Push door upwards to upper lock.

4. CUT-IN

a. Use the skin penetrator, power rescue saw, or crash ax as applicable. See 6 zones.

DOUBLE TRACK SLIDE

SINGLE TRACK SLIDE

4aCUT-IN ZONES

TOOPEN

a

b

e

f

c

d

h gPUSH

OPEN

CLOSED

FRONT AND AFTCARGO DOOR-RIGHT SIDE

FRONT, AFT, ANDEMERGENCY EXITS(EXTERNAL ENTRY)

BULK DOOR

AIRBUS A310-300T.O

. 00-105E-9

AIR

BU

S A

310-300.4

ENGINE AND APU SHUTDOWN1. ENGINE SHUTDOWN

a. Place throttle levers, located on center pedestal, to AFT position.

b. Push fuel levers, located aft of throttles, to DOWN position.

c. Pull both emergency engine shut off valve handles, located on left overhead panel.

d. Place APU shutdown switch, located on forward center overhead panel, on OFF position.

e. Pull emergency APU shut off valve, located on center of overhead panel.

f. Press battery switches, located on right center overhead panel, to OFF position.

2. APU SHUTDOWN ON GROUND

a. Open APU shutters, located at nose wheel or panel between main landing gear.

b. Press APU pushbutton to ON position.

1aTHROTTLES

1bFUEL LEVERS

1cENGINE #1SHUT OFF VALVE

1fBATTERY SWITCHES

1eAPU SHUT OFFVALVE

1cENGINE #2SHUT OFF VALVE

1dAPU SWITCH

2aAPUSHUTTERS

2bAPUPUSHBUTTON

2bAPUPUSHBUTTON

AIRBUS A310-300T.O

. 00-105E-9

AIR

BU

S A

310-300.5

AIRCREW EXTRACTION,SLIDE DEPLOYMENTAND ESCAPE ROUTES1. AIRCREW EXTRACTION

a. Disconnect lap belts and shoulder harnesses from crew members and flight crew members.

b. Disconnect lap belts from passengers.

2. SLIDE DEPLOYMENT-INTERNAL

a. Set arming lever, located on front, aft and wing exits, to ARMED position.

b. Hold and lift opening door handle. Front and aft doors have a system that assist their opening.

c. Push wing exits from up to down.

3. MANUAL SLIDE INFLATION-INTERNAL

a. In case of non automatic inflation, pull handle at base of door opening.

4. ESCAPE ROUTES

a. Follow arrows for double and single track slides on both sides of fuselage.

2a, 2bFRONT AND AFT DOORS

2a, 2cWING EXITS

2bOPENING HANDLE

2aARMING LEVER

3aMANUAL HANDLE

4aESCAPE ROUTES USINGDEPLOYED SLIDES

AIRBUS A310-304T.O

. 00-105E-9

AIR

BU

S A

310-304.

The aircraft information is pending release.

1

AIRBUS A340-500/600T.O

. 00-105E-9

AIR

BU

S A

340-500/600. 1

AIRCRAFT COMPOSITE MATERIALSCARBON FIBER REINFORCED PLASTIC (CFRP)

ARIMID FIBER REINFORCED PLASTIC (AFRP)

GRAPHITE FIBER REINFORCED PLASTIC (GFRP)

HYBRID (GRAPHITE + CARBON) WING TIP FENCES

AILERONS

FLAP TRACK FAIRINGS

OUTER FLAPFIXED LEADING EDGE UPPERAND LOWER PANELS

BELLY FAIRING SKINS

PRESSURE BULKHEAD

VERTICALSTABILIZER

HORIZONTALSTABILIZEROUTER BOX

APRON

KEEL BEAM

OVERWINGPANEL

TRAILING EDGE UPPER AND LOWER PANELSAND SHROUD BOX

SPOILERS

RADOMENOSE LANDINGGEAR DOORS

MAIN AND CENTERLANDING GEAR DOORS

PYLON FAIRING ANDNACELLES COWLINGS

MAIN LANDING GEARLEG FAIRING DOOR

AVIOCAR 212T.O

. 00-105E-9

AVIO

CA

R 212.1

The aircraft information is located in Chapter 6 containing US Air Force aircraft.

BAE 146T.O

. 00-105E-9

BA

E 146. 1

AIRCRAFT HAZARDSOTHER HAZARDS:Battery acidAsbestosBeryllium + beryllium oxidesBromochlorodifluoromethane (BCF Fire Extinguishant)Bomotrifluoromethane (BTM Fire Extinguishant)Cartridge operated equipmentDimethylformamide (Strobe power pack)Ejector Release Units (ERUs)Lithium (Batteries)Polytetrafluoroethylene“SKYDROL” Hydraulic Oil OX-20Sonar locator beacon(s) (1-Lithium battery)Tritium Light Sources (Beta Lights)Fuel: AvturHydraulic oil: OM-15/OX-20High pressure gases: NitrogenEngine oil: OX-27Oxygen: Gaseous

WINGVENTTANK

INTEGRALWINGFUELTANK INTEGRAL

CENTERFUEL TANK

OPTIONALPANNIERTANKS

APU FIRE EXINGUISHERHAND FIRE EXINGUISHER BCF

PORTABLE OXYGEN BOTTLE

INTEGRAL WING FUEL TANK

WING VENT TANK

FUSIBLE PLUGS ON MAIN WHEELS3 PER WHEEL

FIRE ACCESS PANELS2 PER ENGINE

ENGINEFIREBOTTLES2 PER ENGINEBTM

HYDRAULIC FLUIDRESERVOIRS TYPE 4 PHOSPHATE ESTER FLUID

HAND FIREEXINGUISHERBCF

BATTERY

MAIN OXYGEN BOTTLE1.870 LITRES

TORCH & TOGGLE BOX

AX

SMOKE MASK STOWAGE

PORTABLE OXYGEN BOTTLES

HAND FIRE EXINGUISHERS

REFUEL PANEL

BAE 146T.O

. 00-105E-9

BA

E 146.

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxAIRCRAFT ENTRY

1. FORWARD & AFT SERVICE DOORSa. Pull handle out, to fullest extent, rotate clockwise to open door. Doors are located on right side fuselage.

2. AFT CARGO BAY DOORa. Twist handle to “UNLOCK”, then push door inwards. Door is located aft of main landing gear on right side fuselage.

3. FORWARD CARGO BAY DOORa. Twist handle to “UNLOCK”, then push door inwards. Door is located forward of main landing gear on right side fuselage.

4. OTHER DOORSa. To open avionics bay door, located under forward service door, twist handle to “UN- LOCK”, then push door inwards.b. To open hydraulics bay door, located just aft of forward cargo bay door, twist handle to “UNLOCK”, then push door inwards.c. To open air conditioning bay door, located forward of the APU bay door, release two latches to lower door outwards.d. To open APU bay door, located forward of tail cone, release three latches to lower door outwards.

5. WINDOW PANEL EXITa. Panel opens from inside inwards left and right. Escape ropes are located near panel.

6. CUT-INa. Cut-in where fuselage is marked. See illustrated marking.

2

5aESCAPE ROPESTOWAGE

5aWINDOWPANELEXIT

CUT HERE INEMERGENCY

BREAK INRESCUE PANELS

1aFORWARD &AFT SERVICEDOORS

6aCUT-INAREAS

2aAFT CARGOBAY DOOR

3aFORWARD CARGOBAY DOOR

4aAVIONICS BAY DOOR

4bHYDRAULICSBAY DOOR

4dAPU BAY DOOR

4dAPU LATCH(TYPICAL)

TWISTHANDLE(TYPICAL)

BAE 146T.O

. 00-105E-9

BA

E 146.3

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN

a. Slide baulk release down and move thrust levers/High Pressure valve, located on center pedestal, back to fullest extent to CLOSE.

b. For fire engine handles 1, 2, 3, and 4, located on center overhead panel, pull through rotary baulk to fullest extent (4.75”) to close Low Pressure valve.

c. Place battery switch, located left center overhead panel, down to OFF.

d. Depress pilot’s brake pedals, located aft of thrust levers, simultaneously and pull to park on “YEL”, release brake pedals.

e. Turn oxygen system isolation valve, located on right console, to OFF.

NOTE: APU emergency shutdown switches are located at rear of air conditioning bay access and at refuel panel.

2. AIRCREW EXTRACTION

a. Disconnect seat belts and shoulder harness from crew members.

b. Disconnect seat belts from passengers.

1aTHRUST LEVERS/HIGH PRESSURE VALVE

1bFIRE ENGINEHANDLES

1cBATTERYSWITCH

1eOXYGEN SYSTEMISOLATION VALVE1d

PARK BRAKELEVER

BN 2AT.O

. 00-105E-9

BN

2A. 1

AIRCRAFT DIMENSIONS

WING SPAN 49’ 0” (14.94 M)

HEIGHT 13’ 8.75” (4.18 M)

LENGTH 35’ 7.75” (10.86 M)

BN 2AT.O

. 00-105E-9

BN

2A.

2

INTEGRALFUEL TANK

INTEGRALFUEL TANK

SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash Ax

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Use three entry doors to gain access to aircraft. Two doors located on the left side and one door located on the right side of fuselage.

b. Aircraft accomodates ten personnel. Seats are mounted side by side, no aisles. Seat backs fold forward. Access to all seats are through the three entry doors.

2. EMERGENCY ENTRY AND EXITS

a. Use three entry doors for emergency entry or exit.

b. Cargo door, located on aft right side of fuselage may also be used as an emergency exit by removing door/window.

3. OTHER CONFIGURATIONS

a. During entry, rescue personnel may encounter aircraft configurations consisting of passenger, freighter, photographic, geophysical survey, parachutist transport (8 parachutists with 1 dispatcher), trainer, firefighting, environmental protection, cropspraying, or amulance with up to 3 stretchers and two attendants.

4. CUT-IN

a. If doors are inoperable, use power rescue saw or crash ax to gain access.

TOTAL INTEGRALFUEL TANKS CAPACITY137 US GAL (518 LITRES)

WING TIPFUEL TANK

WING TIPFUEL TANK

WITH WING TIP FUEL TANKSCAPACITY INCREASED TO215 US GAL (814 LITRES)

OPTIONAL PYLON MOUNTED UNDER-WINGAUXILIARY FUEL TANKSEACH TANK 60 US GAL (227 LITRES)

OIL CAPACITY:6 US GAL (22.75 LITRES)

BATTERY: 24 V 25 AHHEAVY DUTY LEAD ACID

2bCARGO DOOR

1a, 2aENTRY DOOR1a, 2a

ENTRY DOOR

1a, 2aENTRY DOOR

BN 2AT.O

. 00-105E-9

BN

2A.


a. Place four (4) engine magneto switches, located on left overhead panel, to the OFF position.

b. Place two (2) fuel cock selectors, located on the center overhead panel, to the OFF position.

c. Place the battery/alternators switch, located on the pilot’s lower forward panel, to the CUT-OFF position.


a. Disconnect crew and passenger lap belts and shoulder harnesses as applicable.

3

1bFUEL COCKSELECTORS

1aENGINEMAGNETOSWITCHES

1cBATTERY/ALTERNATORSSWITCH

C-20/HT.O

. 00-105E-9

C-20/H

.1


C-27A/G222

T.O. 00-105E

-9

C-27A

/G222.1


C-31A/F-27 T.O. 00-105E

-9

C-31A

/F-27.1


C-47T.O

. 00-105E-9

C-47.1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Rotate door handle, located on main cabin entrance door, clockwise, then open door outward.

b. Pull door handle, located on pilot’s compartment door, down, then open door outward.

2. EMERGENCY ENTRY

a. Pull emergency exit external handle, located on emergency hatch aft of wing, each side of fuselage, to unlock, then pull emergency exit hatch outward.

b. Rotate pilot’s escape hatch handle, located forward top center of fuselage, clockwise, then pull hatch up and aft.

3. CUT-IN

a. Cut-in area are located at normal and emergency entrance points and at pilot’s windows, left and right side of flightdeck.

PORTABLEOXYGENBOTTLES

BATTERIES

400 GAL

FLARE LAUNCHER

AMMUNITION

AC-47D GUN POSITIONS

OXYGEN CYLINDERS

AC-47D FIRECONTROLBOX

(INSTALLEDFOR FERRYING)

400 GAL

2aEMERGENCY EXIT HATCH

3aCUT-IN

1aMAIN CABINENTRANCE DOOR

2bPILOT’SESCAPEHATCH

1bPILOT’SCOMPARTMENTDOOR

C-47T.O

. 00-105E-9

C-47. 2

1. ENGINE SHUTDOWN

a. Retard throttle control levers, located between pilot’s and co-pilot’s seat, to full CLOSE position.

b. Place mixture control levers, located between pilot’s and co-pilot’s seats, to the aft CUT- OFF position.

c. Turn master ignition switch, located on center overhead panel, to OFF position.

d. Turn battery switch, located on overhead switch panel, to OFF position.

NOTE: If engines fail to shutdown, pull firewall shutoff valve handle, located on engine fire extinguisher control panel, OUT.


a. Unlatch lap belt and remove shoulder harness from crewmember(s).

NOTE: If seat tracks are not damaged during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).

ENGINE SHUTDOWN ANDAIRCREW EXTRACTION

1aTHROTTLECONTOLLEVERS

1bMIXTURECONTROLLEVERS

1cMASTERIGNITIONSWITCH

SEATCONTROLHANDLE

FIREWALL SHUTOFFVALVE HANDLE

ENGINE FIREEXTINGUISHERCONTROL PANEL

1dBATTERYSWITCH

C-130/T-10 T.O. 00-105E

-9

C-130/T

-10.1


C-130HT.O

. 00-105E-9

C-130H

.1 FUEL F349670 US GAL (36600 LITRES)

3M

BATTERY GASEOUS OXYGEN2 X 568 US GAL (2 X 2152 LITRES)

BLAST UP TO98 FT (30 M)37 KT (69 KM/H)

AIRCRAFT DIMENSIONSWING SPAN 133’ (40.5M)LENGTH (C-130H) 98’ (29.8M) (C-130H 30) 113’ (34.3M)HEIGHT 38.3’ (11.68M)


AIRCRAFT ENTRY

NOTE: For more information about the C-130, go to Chapter 6. The information in these procedures also include the C-130H30 model.

1. NORMAL ENTRY

a. To open crew door, located forward left side of fuselage, turn door handle counterclockwise.

b. To open paratroop doors, located aft of engines on right and left side of fuselage, turn door handle clockwise, then push in and lift up the door.

2. EMERGENCY ENTRY

a. To open side emergency doors, located forward of engines right and left sides of fuselage, press button, turn handle, and then push door inside of aircraft.

b. To open aft escape hatches, located over flight deck, between wings, and forward of vertical stabilizer, lift and pull up ring, then push hatch in. Be careful not to drop hatch on personnel.

3. CUT-IN

a. Cut-in areas may or may not be designated by markings. Cut in to areas only marked to prevent cutting into high pressure lines with flammable fluids such as hydraulic lines.

2bESCAPE HATCHESWITH RING

1aCREWDOORHANDLE

1bPARATROOPDOORS WITHHANDLE

2a SIDE EMERGENCY DOORS WITH HANDLE

2aDOOR BUTTON

OPEN

LOCKED

C-130HT.O

. 00-105E-9

C-130H

. 2

ENGINE AND OXYGEN SHUTDOWN1. ENGINE SHUTDOWN

a. Pull all four engine shutdown T-handles, located on center overhead panel.

b. Pull APU shutdown handle, located on center overhead panel right of engine shutdown T-handles.

c. Set electric power shutdown switch, located on center overhead panel right side, to OFF position.

d. Close oxygen cocks, located in compartment in front of crew door, to CLOSE position.

1aENGINET-HANDLES

1bAPU T-HANDLE

1cELECTRICPOWERSWITCH

1dOXYGENCOCKS

C-130HT.O

. 00-105E-9

C-130H

.3

AIRCREW EXTRACTIONAND ESCAPE ROUTES1. AIRCREW EXTRACTION- SEAT COMPONENTS

a. Adjustable headrest

b. Tip-up armrest

c. Thigh support control

d. Front-rear horizontal setting lever

e. Harness winding locking lever

f. Lumbars horizontal support setting

g. Lumbars vertical support setting

h. Back seat inclination lever

i. Height setting lever

j. Seat rotation lever

1a

1a

1a

1a

1b

1b

1b

1b

1c

1c

1d

1d

1e

1e

1f

1f

1g

1g

1h

1h

1i

1i

1j

CARGO DOORAND RAMP

ESCAPE ROUTES

NAVIGATORAND FLIGHTENGINEER’SSEAT

PILOT’SSEAT

C-135T.O

. 00-105E-9

C-135.1


C-135FRT.O

. 00-105E-9

C-135F

R. 1

SPECIAL TOOLS/EQUIPMENTPower Rescue SawSkin Penetrator Tool24 Foot LadderCrash Ax

AIRCRAFT ENTRYNOTE: Entry procedures for the C-135FR have not been provided. Consult Segment 1 for the C-135 information.

OXYGEN ANDCONVERTERS

OXYGENVALVE

OXYGENCONVERTER

BATTERIES

FUEL LOADAPPROX. 27,810 GALS(105,241 LITERS)

ESCAPE ROUTES(CARGO OPENSINTERNALLY) AFT DOOR

CREWENTRANCE

CARGO DOOR

EMERGENCY ESCAPE HATCH(BOTH SIDES)

C-135FRT.O

. 00-105E-9

C-135F

R.2


NOTE: General shutdown of electric and fuel circuits.

a. Pull the four (4) flame arrester valves “C.F.”, located on windshield panel, to shut down fuel and hydraulic fluid, as well as all battery power.

b. Set battery switch, located left of flame arrester valves, to OFF, to obtain general shutoff of electric circuits.

c. Move power levers aft, lifting levers to override the idle stop.


a. Disconnect lap belts and shoulder harnesses as applicable for crewmembers and passengers.

1aFLAMEARRESTERVALVES

1bBATTERYSWITCH

1cPOWERLEVERS

C-140T.O

. 00-105E-9

C-140. 1

SPECIAL TOOLS/EQUIPMENTPower Rescue SawSkin Penetrator ToolCrash Ax

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Pull exterior door handle, located left forward side of fuselage, out and turn clockwise.

b. Extend stairway downwards by releasing the locking latch, located left top of stairway frame, and slide stairs forward to stop position. Lower stairs outward.

2. EMERGENCY ENTRY

a. Push external plate, located left and right side over wing, to open emergency escape windows. Use caution while pushing inward.

NOTE: Some C-140 models have four emergency escape windows. Only the right front forward window is equipped with a foldout step.

3. CUT-IN

a. Cut in areas as marked on fuselage and engine cowlings. (See skin penetration locations.)

OXYGEN CYLINDERS(Two fixed in baggagecompartment. Oneportable in flightcompartment.)

FUELTANKS

CAUTION

Unaniferous balance weight isintegrated in top of rudder unit.Under influence of fire or greatheat, radioactivity may be exposed.

BATTERIES(Under baggagecompartment flooron right side.)

3aSKINPENETRATIONPOINTS

3aCUT-IN

2aEXTERNALRELEASEPLATE

1a, 1bEXTERIORDOOR WITHSTAIRWAY

NO ARMAMENT IS CARRIED

FUEL TANK CAPACITIES:OUTBOARD WING: 375 GAL (1419.11 LITRES)INBOARD WING: 390 GAL (1648.92 LITRES)WING TANK: 565 GAL (2388.82 LITRES)

C-140T.O

. 00-105E-9

C-140.2

ENGINE SHUTDOWN1. NORMAL ENGINE SHUTDOWN

NOTE: If flight mechanic seat is occupied and/or in position, release seat prior to performing engine shutdown.

a. Retard throttle levers, located on center console, to IDLE position, then raise and move aft to OFF position.

b. Place battery switch and power select switch, located on overhead engine start panel, to OFF position.

2. EMERGENCY ENGINE SHUTDOWN

a. Pull fire emergency T-handles, located on upper center instrument panel.

b. Place battery switch and power select switch, located on overhead engine start panel, to OFF position.

1aTHROTTLELEVERS

1bBATTERYSWITCH2a

FIRE EMERGENCY HANDLES

ENGINE START PANEL

CENTER CONSOLE

ENGINE START

FIRE WARNING STEADY LIGHT FLASHING LIGHT ENG FIRE FWD ZONE OVERHEAT AFT ZONE

FIRE 1 PULL FIRE 2 PULL FIRE 3 PULL FIRE 4 PULL

C-140T.O

. 00-105E-9

C-140.3

AIRCREW EXTRACTION1. AIRCREW EXTRACTION

NOTE: If seat tracks are not damage during crash landing, use adjustable seat control to retract seats to aft position in removing crewmember(s).

a. Pull seat lock control release lever, located under right side of seat, downward to release seat from its locked position.

b. Release lap belt and remove shoulder harness from crewmember(s). Release is a rotating buckle type.

c. Passenger seats are equipped with lap belts only. Unlatch lap belt from passenger(s).

1aSEAT LOCK CONTROLRELEASE LEVER

FLIGHTMECHANIC’SSEAT

1bLAP BELTRELEASE

PILOT’SSEAT

C-160 TRANSALL ASTARTET.O

. 00-105E-9

C-160TA

.1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. For the crew door, located forward left side fuselage, push door shutter, then pull door lever.

b. For the paratroop doors, located aft of wing roots, pull ring, press button, rotate handle, then lift up door.

2. EMERGENCY ENTRY

a. For side emergency door, located on forward right side fuselage, pull ring, press button, rotate handle, then push door inward.

b. For top aft emergency hatches, located at base of vertical stabilizer, pull ring, press button, rotate handle, then push door inward.

NOTE: Do not drop hatches inside cockpit or aft compartment section. Falling hatches can endanger crewmembers (if installed) or passengers.

3. CUT-IN

a. Cut in panels for emergency rescue.

FUEL F.34TOTAL 4990 GAL(18960 LITRES)

BATTERY

CREW GASEOUS OXYGEN1011 US GAL (3828 LITRES) PASSENGER GASEOUS

OXYGEN 1650 US GAL(6246 LITRES) BATTERY

SF6 4.4 LB(2X2KG)

APU

H515 HYDRAULIC OIL 5 US GAL &2 x 6.34 US GAL(19.1 CT 2X23 LITRES)

S.1774METHANOL - WATER 100 US GAL (380 LITRES)

2aSIDE EMERGENCY DOOR

2bTOP AFTEMERGENCYHATCHES


1bPARATROOP DOOR

1aCREW DOOR

1aDOOR LEVER

1aDOORSHUTTER

NO ARMAMENTIS CARRIED


. 00-105E-9

C-160TA

.2

ENGINE SHUTDOWN1. ENGINE SHUTDOWN

a. Pull both throttle levers, located on center console, to AFT position.

b. Pull both fuel levers, located on center console right of throttle levers, to AFT position.

c. For APU shutdown, press on both APU buttons, located upper right center console, then press on APU switch to cut off right APU fuel.

d. For fuel cut off, switch off cocks for fuel tanks, then bring levers to AFT position. DO NOT MANIPULATE YELLOW AND BLACK LEVER.

e. For engine and APU fire extinction, pull engine fire switches, located on center overhead panel, then turn switches to left or right to deliver extinguisher agent.

f. For electric power cut off, pull down crash bar, located on upper left overhead panel, to OFF position.

1dFUEL COCKLEVERS

1dFUEL COCKLEVERS

1dYELLOW/BLACK LEVER (Do not manipulate.)

1aTHROTTLELEVERS

1bFUEL LEVERS

1fCRASH BAR

1eFIREENGINEHANDLE

1cAPU FUELSWITCH

1cAPUBUTTONS

1eAPUENGINEHANDLES

1eFIREENGINEHANDLE


. 00-105E-9

C-160TA

.3

AIRCREW EXTRACTION,CABIN CONFIGURATIONAND ESCAPE ROUTES1. AIRCREW EXTRACTION

NOTE: Navigator and loadmaster, sitting right beside the staircase, are secured by seat belts, all other crewmembers are secured by a seat belt and harness strap combination.

a. Unlatch quick releases of seat belts and remove belt straps from navigator and loadmaster.

b. In the cockpit, pull seat lock control release lever located right side of flight engineer’s seat aftwards, to release seat from its locked position. Move seat aftwards to stop position. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract flight engineer.

c. Unlatch seat lock control release pedal, located left side of co-pilot’s seat, to release seat from its locked position. Move seat aftwards to stop position. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract co-pilot.

d. Pull seat lock control release lever, located left side of pilot’s seat aftwards, to release seat from its locked positiion. Move seat aftwards to stop position and rotate seat to the left towards stair case. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract pilot.

NOTE: Passengers and crew may not exceed 18 personnel.

1aNAVIGATOR AND LOADMASTER SEAT BELT

1b, 1c, 1dPILOT, CO-PILOT, AND FLIGHT ENGINEER SEATBELT AND HARNESS STRAP COMBINATION

ESCAPE ROUTES

TACTICALZONE

CREW ZONE REST AND TECHNICAL ZONE

CABIN CONFIGURATION

C-160 TRANSALL GABRIELT.O

. 00-105E-9

C-160T

G. 1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. For the crew door, located forward left side fuselage, push door shutter, then pull door lever.

b. For the paratroop doors, located aft of wing roots, pull ring, press button, rotate handle, then lift up door.

2. EMERGENCY ENTRY

a. For side emergency door, located on forward right side fuselage, pull ring, press button, rotate handle, then push door inward.

b. For top aft emergency hatches, located at base of vertical stabilizer, pull ring, press button, rotate handle, then push door inward.

NOTE: Do not drop hatches inside cockpit or aft compartment section. Falling hatches can endanger crewmembers (if installed) or passengers.

3. CUT-IN

a. Cut in panels for emergency rescue.

FUEL F.34 7188 GAL(17188 LITRES)

BATTERY

CREW GASEOUS OXYGEN1062 US GAL (440 LITRES+SECOURS 150 LITRES)+EMERGENCY 40 US GAL

BATTERY(NACELLE)

0159 CARGO RAMPRESERVOIR 2.64 US GAL(10 LITRES)

APU

H515 HYDRAULIC OIL

5.28 + 5.28 US GAL(20.1 + 20.1 LITRES)

S.1774METHANOL - WATER44/56 84.5 US GAL (320 LITRES)


2bTOP AFTEMERGENCYHATCHES


1bPARATROOP DOOR

1aCREW DOOR

1aDOOR LEVER

1aDOORSHUTTER

NO ARMAMENTIS CARRIED


. 00-105E-9

C-160T

G. 2


a. Pull both throttle levers, located on center console, to AFT position.

b. Pull both fuel levers, located on center console right of throttle levers, to AFT position.

c. For APU shutdown, set air intake valve switch to CLOSE position.

d. For fuel cut off, switch off cocks for fuel tanks, then bring levers to AFT position. DO NOT MANIPULATE YELLOW AND BLACK LEVER.

e. For engine and APU fire extinction, pull engine fire switches, located on center overhead panel, then turn switches to left or right to deliver extinguisher agent.

f. For electric power cut off, pull down crash bar, located on upper left overhead panel, to OFF position.

1dFUEL COCKLEVERS

1dFUEL COCKLEVERS

1dYELLOW/BLACK LEVER (Do not manipulate.)

1aTHROTTLELEVERS

1bFUEL LEVERS

1fCRASH BAR

1cAPU AIRINTAKESWITCHPANEL

1eFIREENGINEHANDLE

1eFIREENGINEHANDLE

1eAPUENGINEHANDLES


. 00-105E-9

C-160T

G. 3

AIRCREW EXTRACTION,CABIN CONFIGURATIONAND ESCAPE ROUTES1. AIRCREW EXTRACTION

NOTE: Navigator and loadmaster, sitting right beside the staircase, are secured by seat belts, all other crewmembers are secured by a seat belt and harness strap combination.

a. Unlatch quick releases of seat belts and remove belt straps from navigator and loadmaster.

b. In the cockpit, pull seat lock control release lever located right side of flight engineer’s seat aftwards, to release seat from its locked position. Move seat aftwards to stop position. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract flight engineer.

c. Unlatch seat lock control release pedal, located left side of co-pilot’s seat, to release seat from its locked position. Move seat aftwards to stop position. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract co-pilot.

d. Pull seat lock control release lever, located left side of pilot’s seat aftwards, to release seat from its locked positiion. Move seat aftwards to stop position and rotate seat to the left towards stair case. Pull red release snap from harness quick release box until straps are released. Lift left armrest upwards and extract pilot.

NOTE: Passengers and crew may not exceed 20 personnel.

1aNAVIGATOR AND LOADMASTER SEAT BELT

1b, 1c, 1dPILOT, CO-PILOT, AND FLIGHT ENGINEER SEATBELT AND HARNESS STRAP COMBINATION

CREW ZONE REST ZONE TACTICAL ZONE REAR ZONE AND TAIL

CABIN CONFIGURATION AND ESCAPE ROUTES

WINDOWS AND EMERGENCY HATCHES EQUIPPED WITH ESCAPE ROPES

CC-138/UV-18A/B T.O. 00-105E

-9

CC

-138/UV

-18A/B

.1


CC-142/E-9AT.O

. 00-105E-9

CC

-142/E-9A

.1


CC/CE/CP-144T.O

. 00-105E-9

CC

/CE

/CP

-144.1


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Push button on cabin entry door handle, located on forward left side of fuselage. Handle will extend outward for rotation.

b. Turn cabin door handle counterclockwise to unlock door.

c. Pull cabin door outward.

2. EMERGENCY ENTRY

a. Push in flap on emergency entrance door, located on right side of fuselage over right wing.

b. Push door inward. Be careful of passengers while pushing door. Do not block entrance with door.

3. CUT-IN

a. Cut-in where applicable, normally around cabin windows.

NOTE: Aircraft accomodates a two pilot flight deck. Cabin seats 19 passengers. Seats will have typical restraint systems.

1aPUSH BUTTON

PUSH

1bCABIN DOORHANDLE LOCKED

UNLOCKE

D

EMERGENCY ENTRANCE

PUSH IN FLAP

DOOR DOOR INWARD

2aFLAP

2bEMERGENCYENTRANCE

AIRCRAFT DIMENSIONSWING SPAN 64’4” (19.61 M)LENGTH 68’ 5” (20.85 M)HEIGHT 20’ 8” (6.30 M)

CC/CE/CP-144T.O

. 00-105E-9

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/CE

/CP

-144. 2

FIRE FIGHTING HAZARDS

INTERNAL ENGINE FIRE ENGINE EXHAUSTNOZZLE FIRE

BRAKE FIRE

REAR EQUIPMENTBAY FIRE

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AIRCRAFT PAINT SCHEME

1

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AIRCRAFT DIMENSIONS

HEIGHT 26.8 FEET(8.17 METERS)

LENGTH 70.2 FEET(21.40 METERS)

WING SPAN 84.6 FEET(25.81 METERS)

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AIRCRAFT CHARACTERISTICS

3 MISSION: Tactics and Logistics Transport

CREW: 1 Pilot, 1 Co-Pilot, 1 Navigator- FlightEngineer

PASSENGERS:48 Troops33 Parachutists with equipmentLitters (+ 4 sanitaries) 21

HEIGHT UNDER PROPELLERS: 1.59 Meters

FUEL:

· Flash Point: 51°C· Reservoir: 5,260 litres

LIQUID HYDRAULIC: H 515

· Flash Point: 91°C· Reservoir : 10 litres· Complete Circuit or Loop: 25 litres

ENGINE OIL: O156

· Flash Point: 268°C· (2 x 6,9 litres) : 13.8 litres

OXYGEN (gas):

· Crew Cabin Circuit:1,441 litres· Pilot Emergency Bottle: cabin 620 litres· Portable Emergency Bottles: (3x312 l)

936 litresTo open the access by pulling inwards on thespring loaded handles “A”. To shut the circuitoff, turn the handle “B” toward off. The oxygencircuit only feeds the cockpit.

MAXIMUM WEIGHT (at takeoff): 16,500 kg

ROLLING DISTANCE:

· At takeoff: 500 at 1100 m· At landing: 700 at 900 m

BRAKES: aluminium alloy rotors

FUEL

BATTERIES

OIL

OXYGEN

HYDRAULIC

BATTERY COMPARTMENT ACCESS IS ON EACH SIDE OF THE AIRCRAFT

BATTERY AND DISCONNECT - CUT BREAK WIRE, UNSCREW & PULL HANDLE “B”

OXYGEN COMPARTMENT ACCESS OXYGEN BOTTLE

“A”

“B”

“B”

CN 235T.O

. 00-105E-9

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AIRCRAFT MATERIALS AND FIREEXTINGUISHER LOCATIONSAGENTS EXTINCTEURS PRECONISES :

· Brake pads : BC powder· Light metals : BC powder· Pneumatics : Water spray· Engines : CO2

ENGINE COMPARTMENTS EXTINGUISHING AGENT:BCF (halon 1211), (2x 2 kg) 4 kg

4

AX

HALON FIRE EXTINGUISHER

WATER FIRE EXTINGUISHER

FIBER WITH RESIN COMPOSITE

CARBON COMPOSITE

CN 235T.O

. 00-105E-9

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AIRCRAFT HAZARDSFRONTAL PROPELLER DANGER ZONE 3 METERS

SIDE PROPELLER DANGER ZONE

ENGINE EXHAUST DANGER ZONE

1. AIRCRAFT HAZARDS FORPROPELLERS AND ENGINES

NOTE:Specific fire access areas for theengines does not exist. Fire extinguish-ing agents must be sprayed into theengine compartment through the ventila-tion openings. The red circled areasdenotes the maintenance access only.

5

SIDE PROPELLER DANGER ZONE

FRONTAL PROPELLER DANGER ZONE 3 METERS

LH ENGINE ACCESS RH ENGINE ACCESS

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SPECIAL TOOLS/EQUIPMENTPower Rescue SawAx

1. AIRCRAFT ENTRY

a. To open the crew entry door, push button andpull handle. The door, when opened, willexpose the door mounted ladder allowing entry.

2. EMERGENCY EXIT

a. To open emergency exit, push on handle.

b. With exit door handle out, turn in the clockwisedirection of the arrow.

c. Push door.

NOTE:Entry through the crew door or through anemergency exit is to be avoided when enginesare running.

3. JUMP DOORS

a. The jump door consists of two separate halves.To open top half, push on door handle toexpose handle for turning.

b. Turn door handle in the direction of the arrow.

c. Push and slide aft.

d. To open bottom half, unlock interior handle, liftand angle at 45 degrees.

e. Lift door and remove.

4. CABIN WINDOWS

a. Windows may be used as a last resort exit.

6

4aLH & RHWINDOWS

3a, 3b, 3cJUMP DOOR(TYPICAL FOR RH & LH)

EMERGENCY EXIT

CREW DOOR

1aPUSHBUTTON

1aUNLOCKHANDLE

2a, 2b, 2cUNLOCKHANDLE

CN 235T.O

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AIRCRAFT INTERIOR ARRANGEMENTAND EVACUATION ROUTES7

RH CREWWINDOW

LH CREWWINDOW

CREW DOOREMERGENCY EXIT

RH AFTJUMP DOOR

RH EXIT FROMCARGO RAMP DOOR

LH AFTJUMP DOOR

LH EXIT FROMCARGO RAMP DOOR

EMERGENCY EXIT

CREW DOOR

RH AFTJUMP DOOR

LH AFTJUMP DOOR

CN 235T.O

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ENGINE, POWER, ANDENGINE FIRE SHUTDOWN8

1. ENGINE SHUTDOWN

a. On the central instrument panel,located between crewmembers, pullthrottle levers aft.

2. POWER SHUTDOWN

a. Pull and flip the battery switch,located on the overhead panel, downto the OFF position

b. Pull and flip the generator switch,located on the overhead panel, downto the OFF position.

3. ENGINE FIRE SHUTDOWN(IN CASE OF FIRE ONLY)

a. Push button down to unlock thesafety locks.

b. Pull the engine throttles to cut fuelsupply.

c. On the percussion halon extinguish-ers, turn lever L to the left. Turn leverR to the right.

NOTE:The system contains two 2 kgsbottles of halon 1211.

1a, 3bTHROTTLES

2aBATTERYSWITCH

2bGENERATORSWITCH

3aSAFETYLOCKS

3cLEVER L

3cLEVER R

CN 235T.O

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AIRCREW EXTRACTION

9 1. AIRCREW EXTRACTION

NOTE:To allow access to the cockpit, the middle seator Flight Engineer type seat must be removed.

a. Undo the safety harness of the middle seat.

b. Lift and hold the seat, then lower the seat back.

c. Depress lock, lift and hang the seat to thepartition, release the seat and proceed to crewseats.

d. Seat adjustments levers - (1) Armrest (2) SeatLower (3) Safety Harness (4) Seat Front andBack

e. To release safety harness, turn buckle to the leftor right.

1a, 1bMIDDLESEAT &BACK

1cLOCK

1d(1)

1d(3)

1d(4)

1d(2)

1eBUCKLE

SHOULDERHARNESS

LAPBELT

CN 235T.O

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CARGO RAMP OPERATION

10

1. CARGO RAMP OPERATION FROM COCKPIT

NOTE:Opening the cargo door requires the activation ofthe hydraulic system using electric pumps. Allsteps take place on the overhead panel.

a. To activate the electric circuit, move the masterswitch.

b. Power the control panel by using the batteryswitches.

c. Activate the hydraulic pumps by placing thehydraulic switches.

d. Push the button named “hyd press”.

e. Select the location to open the door from thecockpit - move cargo door switch toward thebottom to open and toward the top to close thedoor.

2. CARGO RAMP OPERATION FROM CARGOAREA PANEL

a. Move cargo door switch toward the bottom toopen the door, toward the top to close the door.Controls are located on the left side just aft ofthe jump door.

1a

1b

1c

1d

1e

1f

2aCARGO DOORPANEL ANDSWITCH

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AIRCRAFT ENTRY

1. NORMAL ENTRY

a. Release double section entry door, located left side of fuselage, by pushing exterior handle for release and turning handle counterclockwise.

b. Release sliding bolts, located inside top and bottom of frame of double section entry door.

2. EMERGENCY ENTRY

NOTE: Escape hatches are not removable from fuselage.

Possible injury can result using the cockpit escape hatches for entry when propellers are rotating.

a. Escape hatches are located on both sides of cockpit. Release hatch handle and turn handle clockwise to open.

b. The second window at right side of fuselage can also be used as escape hatch.

c. To open, pull red marked handle out and pull escape hatch open.

3. CUT-IN

a. Cut-in as applicable at windshild and doors.

FUEL TANKS

FUEL TANKS

BATTERY

1a, 1bDOUBLE SIDEDNORMAL ENTRYPASSENGER DOOR

2aESCAPEHATCHES

WARNING

2bESCAPEHATCH

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a. Retard fire handles, located below center console, DOWNWARDS.

b. Place battery and master switches, located left side pilot’s overhead panel, in OFF position.

2. AIRCREW SHUTDOWN

NOTE: Pilot and co-pilot seats aare equipped with a lap belt and harness combination.

a. Pull red release snap from harness quick release box until lap belt and harness straps are released.

1bMASTERSWITCH

1bBATTERYSWITCH

1aCENTERCONSOLE

2aSTRAPS

2aHARNESS QUICKRELEASE BOX

2aRED RELEASE SNAP

DO 28T.O

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AIRFRAME MATERIALSALUMINUM - ALLOY

ALUMINUM - SANDWICH

TITANIUM - ALLOY

TITANIUM - FRAMEWORK, CFRP COVER

CARBON - FIBER REINFORCED PLASTICS (CFRP)

CFRP/KEVLAR

CARBON - FIBER

GLASS - FIBER REINFORCED PLASTICS (GFRP)

3

FOKKER 60T.O

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60.1

AIRCRAFT HAZARDS

LENGTH 88’ 2” (26.87 M)

AIRCRAFT DIMENSIONS

WING SPAN 95’ 1.75” (29 M)

HEIGHT27’ 4.5”(8.34 M)

DANGER AREA: RADAR RADIATION

2400

R= 20’ (6 M)

DANGER ZONES: ENGINES AND PROPELLERS

IDLE POWER

V= 56KM/H27M89’

V=8KM/H2.25 M7.4’

25 C0

0 0 0 037 C 30 C 20 C 15 C

TAKE OFFPOWER

V=96.5KM/H54 M178’

V=120 KM/H44 M145’

V=161KM/H33 M109’

V=241KM/H 27 M 89’

V=8 KM/H 7 M 23’

0M0’

1M3.3’

FUEL: 1356 US GAL 1130 IMP GAL 5136 LITRES

CREW: 3

PASSENGERS: MAXIMUM 45

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60.2

AIRCRAFT HAZARDS-Continued

MAINFUELTANK

MAIN FUEL TANK

OXYGEN BOTTLE& MEGAPHONE

HYDRAULIC RESERVOIR

LAVATORY (FIRE BOTTLEAND OXYGEN BOTTLE)

FIREEXTINGUISHERBOTTLE

HYDRAULICACCUMULATORS

BATTERIES

FIREEXTINGUISHERBOTTLES

FUELCOLLECTORTANK

SERVICEEMERGENCYDOOR

APU

SAFETYPIN SELFPROTECTIONSYSTEM

FIRSTAID KIT

OPERATIONALOXYGENBOTTLE

FIRSTAIDKIT

EMERGENCYOXYGENBOTTLE

AX

FUEL INFORMATIONCOLLECTOR FUEL TANK 13 GAL(49.2 LITRES)INTERNAL MAIN TANKS 678 GAL(1267.5 LITRES) EACH

ENGINE OILLOCATED ON TOP OF FORWARDENGINE NACELLE

PNUEMATIC BOXLOCATED BY MAIN ENTRY DOOR

NO ARMAMENT IS CARRIED

UTILITY TRANSPORT MISSIONS-STAFF-LOGISTIC-TROOP-MEDIVAC-CARGO

APU

FIREEXTINGUISHERBOTTLE

APU AIRINTAKE

APUEXHAUST

SAFETYPIN

MULTI-PURPOSE DOOR

COCKPIT VOICERECORDERANDFLIGHT DATARECORDER

STORESPYLON

SAFETYPINBOX

EMERGENCYEXITS

FUELCOLLECTORTANK

COUNTERMEASURESDISPENSING POD(IF APPLICABLE)

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SPECIAL TOOLS/EQUIPMENTSkin Penetration ToolPower Rescue SawCrash Ax

AIRCRAFT ENTRY

1. SERVICE /EMERGENCY DOOR

a. Lift handle at “PUSH”.

b. Rotate handle counterclockwise to “OPEN”.

c. Pull door outward.

2. MAIN ENTRANCE DOOR

a. Lift door hand at “PUSH”.

b. Turn handle to “OPEN”.

c. Pull door outward. Use caution, door may open rapidly.

3. EMERGENCY ESCAPE HATCHES

a. Push access panel, located on top center of escape hatch, pull hatch outward, and set aside. Enter aircraft.

LARGECARGODOOR

SLIDING WINDOWS OPEN ONLYFROM INSIDE ESCAPE ROPEABOVE SLIDING WINDOWS (INSIDE)

OVERHEADPANEL

MAIN ENTRANCEDOOR

EMERGENCYEXIT

SAFETYPIN BOX

BATTERIES

OPEN

2a

2b

2c

MAIN ENTRANCE DOOR

FORWARD

EXTERNAL CONTROL PANEL

3aESCAPEHATCH

OPEN

1a

1b1c

FORWARD

SERVICE/EMERGENCYDOOR

3aACCESSPANEL

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60.4

AIRCRAFT ENTRY-Continued4. EMERGENCY EXIT

NOTE: Emergency exit is mounted on large cargo door.

a. To enter, push button to release door and pull door outward. Do not block exit area with door.

5. LARGE CARGO DOOR

a. To open, turn handle clockwise to unlock.

b. Turn handle to OPEN.

c. Open door with open switch.

d. To close, lower door with close switch.

e. Turn handle to close.

f. Turn handle to LOCK.

g. Check vent flap, insure closure.

6. MULTI-PURPOSE DOOR

a. Lift the handle and turn.

b. Push the door inwards.

c. Lift the door using grip.

d. Slide the door aft.

7. CUT-IN

a. Cut-in areas are applicable only if indicated on airframe. (Both sides of aircraft.)

CABIN ESCAPE ROUTES

7aCUT-IN AREAS LH/RH SIDES

SKIN PENETRATION AREA

MULTI-PURPOSE DOOR

6aHANDLE

LARGE CARGO DOOR

CLOSE LOCK

VENT FLAP CAUTIONKEEP FINGERS OUT

4aEMERGENCY EXIT

5c, 5dOPEN AND CLOSESWITCH PANELOPEN CLOSE

OPEN

UNLOCK

DOORINSTRUCTIONS

LOCKED/SAFEHANDLE

5gVENTFLAP

5a, 5b, 5e, 5fLOCK/UNLOCKHANDLE

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60.5


NOTE: Configurations may vary.

a. Move gangbar or battery cut-off switch, located on overhead panel, DOWNWARD.

b. Pull emergency shut-off valves, located on upper forward instrument panel, OUT.

c. Move RPM and HPC control handles, located on center console, REARWARD.

d. Turn crossfeed valve control, located on aft portion of center console, OFF.

e. If needed, pull emergency fuel and hydraulic shut-off handles, located on overhead panel, OUTWARD.


NOTE: Crew of two and one observer are located in cockpit. Ejection seats are not used. Seats are equipped with shoulder harnesses and seat belts. Cabin attendant seats may also be equipped with same type restraints.

a. Disconnect shoulder harnesses and seat belts from crewmembers and cabin attendants.

b. Disconnect seat belts from passengers.

1aGANGBAR

1eEMERGENCY FUEL AND HYDRAULIC SHUT-OFF HANDLES

1aBATTERY CUT-OFF SWITCH

OVERHEAD PANEL

1bEMERGENCYSHUT-OFFVALVES

1dCROSSFEED VALVECONTROL

1cRPM AND HPCCONTROL HANDLES

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LEY.1

FUEL TANKS

FUEL TANKS

BAGGAGE DOOR

2aEMERGENCY EXIT

2bEMERGENCY EXIT

1aPASSENGERENTRANCEDOOR

2bSLIDING WINDOW (BOTH SIDES)

1bCREW/FREIGHT DOOR


AIRCRAFT ENTRY

1. NORMAL ENTRY

a. For passengers, enter through the passenger entrance door, located on the aft left side of the fuselage.

b. For crew members, enter through the crew/freight door on the forward left side of the fuselage.

2. EMERGENCY ENTRY

a. Remove emergency exits, located on each side over the wing, by turning the external handle.

b. Flight deck sliding windows can be used by crew members for evacuation. Windows must be unlocked internally.

3. CUT-IN

a. Cut-in fuselage as required.

OTHER HAZARDS:Battery acidAsbestosBromochlorodifluoromethane (BCF Fire Extinguishant)Cartridge operated equipmentFluorolastomers (Burnt seals)LeadPolychlorinated Biphenyls (PCBs)Water MethanolHalon (Fire Extinguishant)Fuel: JP-8Hydraulic oil: H-515High pressure gases: Air/NitrogenEngine oil: O-149Oxygen

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a. Pull the high pressure cock control levers, located on the center console, aft to the OFF position.

b. Turn both battery switches, located on upper right overhead panel, to the OFF position.


a. Disconnect crew member’s lap belt and shoulder harness.

b. Disconnect passenger’s lap belt.

1aHIGH PRESSURECOCK CONTROLLEVERS

1bBATTERY SWITCHES

HU-16BT.O

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-16B.1

AIRCRAFT HAZARDS

OXYGEN

PROPELLERS

BATTERY FUELTANKS

PROPELLERBLAST

ROCKETS,BOMBS ORTORPEDOES

ROCKETS,BOMBS ORTORPEDOES

RIGHT WING LEFT WING

HU-16BT.O

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HU

-16B. 2


AIRCRAFT ENTRY

1. NORMAL ENTRY

NOTE: The main entrance door consists of an upper and lower section with door release handles on each section.

a. Rotate upper section handle of main entrance door, located on left rear side of fuselage, up and swing door in.

b. Reach inside aircraft and rotate lower section handle, located at top center of lower section of main entrance door, down and swing door in.

2. EMERGENCY ENTRY

a. Rotate emergency door handle, located on lower center of emergency door on right hand side of fuselage, and swing door in.

3. CUT-IN

a. Cut-in pilot and co-pilot escape hatches, located above cockpit side windows.

b. Cut-in bow hatch, located on top of nose forward of windshields.

c. Cut-in cargo loading hatch, located on top of fuselage between wing flaps.

d. Cut-in cabin windows, located on both sides of fuselage, as marked.

1aUPPER SECTIONWITH HANDLE

1aMAIN ENTRANCE DOOR

1bLOWER SECTION WITHINSIDE DOOR HANDLE

SWINGS IN AND AFT

SWINGS IN AND DOWN

AFT COMPARTMENT LEFT SIDEINTERIOR LOOKING FUSELAGEFORWARD

EMERGENCY DOOR2aEMERGENCYDOORHANDLE

3bBOWHATCH

3cCARGO LOADING HATCH

3aPILOT’S &CO-PILOT’SESCAPEHATCHES

CUT HERE FOREMERGENCY RESCUE

3dTYPICAL CABINWINDOWCUT-IN AREA

TYPICAL HATCHCUT-IN AREA

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HU

-16B.3


a. Pull throttles, located on overhead control panel, aft to CLOSED position.

b. Pull mixture controls, located on overhead control panel, aft to IDLE CUT OFF.

c. Pull master ignition switch, located on overhead control panel, OUT.

d. Rotate fuel tank selectors, located on overhead control panel, to OFF position.

e. Position battery switch, located in center of main console for HU-16A and B model aircraft and at left of main console for HU- 16B/ASW (1) and (2) aircraft, to OFF postion.

f. Rotate APU fuel shutoff valve, located on forward side of aft cabin bulkhead, to OFF position.


a. Unlatch lap belts and remove shoulder harness from crewmembers.

b. Unlatch lap belts and remove any other applicable restraints from passengers.

1cBATTERYSWITCH

MAIN CENTERCONSOLE HU-16A/B

HU-16B COCKPIT

1dFUEL TANKSELECTORS

1aTHROTTLES

1bMIXTURE CONTROLS 1c

MASTER IGNITION SWITCH

HU-16B/ASW (1) & (2)COCKPIT

1cBATTERYSWITCH

MAIN CONSOLELEFT SIDEHU-16B/ASW (1) & (2)

1fAPU FUELSHUTOFFVALVE

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AIRCRAFT HAZARDSOTHER HAZARDS:Battery acidCartridge operated equipmentDimethylformamide (Strobe power pack)Lithium (Batteries)PolytetrafluoroethyleneSkydrol Hydraulic Oil OX-2Sonar Locator Beacons (Lithium battery)Strontium chromatesWater MethanolFuel: AvturHydraulic oil: OM-15High pressure gases: Nitrogen/AirEngine oil: OX-26Oxygen: Gaseous

Note: Cargo holds may contain hazardous material.

NOTE: No armament is carried.

PORTABLEOXYGEN114 CU.FT.1800 PSI

INTAKEDANGERAREA

ENGINEOIL

FUELTANK 3

FUELTANK2R FUEL

TANK3A

FUELTANK2R

HYDRAULICRESERVOIR

HYDRAULICACCUMULATORS

REAR CARGO HOLD

JETEXHAUSTEFFLUX

ENGINEOIL

HYDRAULICCOMPARTMENT

FUEL TANK 2L (OUTBOARD)

FUEL TANK 2L

RAM AIRTURBINE

FUEL TANK 1

ENGINE OIL

FUELTANK1A

REVERSETHRUSTDANGER AREA(BOTH SIDES& UNDER TAIL)

INTAKE DANGER AREA

BATTERIES

FORWARDCARGO HOLD

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SPECIAL TOOLS/EQUIPMENTPower Rescue SawCrash AxSkin PenetratorHand Crank

AIRCRAFT ENTRY

1. NORMAL ENTRY

a. To open all passenger doors, three each doors located on right and left sides of fuselage, push in buttton and pull down lever. Slide does not deploy when door is open externally.

b. To open cargo doors, two doors located on right side of fuselage, can only be opened with hand crank tool. (A hand crank tool is also stowed on the flight deck.)

2. EMERGENCY ENTRY

a. Open passenger doors.

b. Open cargo doors.

c. To open the flight deck evacuation hatch, located on forward top of aircraft over the flight deck, by pushing button, then lift open. Crew members can be evacuated by the use of an escape rope attached inside the flight deck.

3. CUT-IN

a. Cut-in areas as marked above and below fuselage windows.

BCF FIRE EXTINGUISHERS

FIRST AID KITS

EXTERNALAPU SHUTDOWN &FIRE EXTINGUISHERCONTROLS ACCESS

EXTERNAL VIEW

1a, 2aPASSENGER DOOR(TYPICAL)

MANUAL OPENING(THIS DOOR ONLY)

2cFLIGHT DECKEVACUATIONHATCH WITHESCAPE ROPES

ENGINE FIRE PANELS

DEPLOYEDESCAPE SLIDE(EACH DOOR)

FIRE ACCESS PANEL

3aCUT-INAREAS

1b, 2bCARGODOOR

ENGINEFIREPANELS

1b, 2bCARGODOOR

3aCUT-INAREAS

FWD

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a. Pull throttle levers, located on center console, back to CLOSE.

b. Place fuel and ignition switches, located aft of throttles, to OFF. This also closes the HP fuel valve.

c. In case of engine fire, pull firepull handle, located on upper windshield panel. Fire extinguisher switch is behind handle. Turn switch left or right to extinguish corresponding engine.

d. In case of APU fire, pull APU fire handle, located on flight engineer’s upper left panel.

e. Place battery switch, located on flight engineer’s left center panel, to OFF.

1cENGINE FIREPULL HANDLES

1dAPU FIREPULL HANDLE 1e

BATTERYSWITCH

1aTHROTTLELEVERS

1bFUEL AND IGNITIONSWITCHES

HAND CRANK STOWAGE(FOR DOORS)

FIRST OFFICER(CO-PILOT) CAPTAIN

(PILOT)

FIRST OBSERVERFLIGHT ENGINEER

SECOND OBSERVER

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AIRCREW EXTRACTION

FLIGHTDECK

CREW RESTAREA MAXIMUM NUMBER OF

CREW/PASSENGERS - 270

CREW AND PASSENGER SEATING ARRANGEMENT

HAND TORCHES

ATTENDANT SEATSPASSENGER SEATS (TYPICAL)

CREW SEATS (TYPICAL)

1aROTARYBUCKLE

EXITS-ALLPASSENGERDOORS

1eESCAPE SLIDE

FLIGHT DECKESCAPE HATCH

5 DESCENTESCAPE ROPES

LADDER1dINTERIORCONTROLS


a. Disconnect crew seats by rotating the rotary buckle.

b. Disconnect the attendant seats restraint system at the central release point.

c. Disconnect lap belts on the passenger seats by lifting the central buckle.

d. Evacuate personnel through doors that are operational. Use interior controls and switches if power is still available.

e. Deploy escape slides using interior switches.

NOTE: Five escape ropes are mounted in the flight deck for overhead escape hatch evacuation.

1cBUCKLE

1bCENTRALRELEASEPOINT

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AIRCRAFT HAZARDS

FUEL TANKSFUEL TANKS

OXYGEN

PROPELLER

WATER METHANOL

PROPELLER

PROPELLER BLAST

OXYGEN

PROPELLER BLAST

NOTE: No armament is carried.

NOTE: Fuel capacity is 1332 GAL or 5040.68 Litres.

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AIRCRAFT ENTRY

1. NORMAL ENTRY

a. The main door is operated and locked hydraulically in link motion with the stairway.

b. The external operation of the main entry door is achieved via the stairway control switch and the battery switch located on the external power panel.

c. The internal operation of the main entry door is achieved via the the stairway control switch and lock-unlock lever on the forward attendant panel.

d. There is an external handle, located externally on the flight deck door on the forward right side of the fuselage.

2. OVERWING EMERGENCY EXIT DOORS

a. Manually release latch and pull handle on emergency exit doors, located over right and left wings.

3. GALLEY DOOR AND AFT CARGO DOOR

a. Manually push in at the PUSH HERE button and turn handle from inside and outside.

4. FORWARD CARGO DOOR

a. Door is operated manually from the outside only and by the PUSH HERE button, then turn handle.

5. CUT-IN

a. Cut-in fuselage as required.

1dEXTERNALEMERGENCYHANDLE

2aOVERWINGEMERGENCYEXIT DOORS

1dFLIGHT DECK DOOR

CLOSE

OPEN

PUSH HERETURN HANDLE

1aMAINDOOR

3aGALLEY SERVICE DOOR

3aEXTERIORHANDLE

1bSTAIRWAYCONTROLSWITCH

DOORLATCHUNLOCK

1bEXTERNAL POWERPANEL

1cSTAIRWAYCONTROLSWITCH

UNLOCK LOCK

1cFORWARDATTENDANTPANEL

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a. Position high pressure fuel cock, located on center console, to the OFF position.

b. Position throttle levers, located on center console, to the MINIMUM position.

c. Position fuel booster pump switches to OFF position.

d. Position generator to OFF position.

e. Position battery switch to OFF position.


a. Unlatch lap belts and remove shoulder harness from crewmembers.

b. Unlatch lap belts and remove any other applicable restraints from passengers.

1bTHROTTLE LEVERS

1aHP FUEL COCKS

CENTER CONSOLE

LOW STOP LEVER

FRICTION WHEEL HANDLE

LOCK LEVER

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